Aero-Optics Experimental Techniques.
Abstract
This report summarizes results of a study to determine the most appropriate aerodynamic experimental techniques for gathering data in aircraft boundary layer and shear layer turbulent flow, flow fields. It focuses on two primary techniques: hot-wire anemometry and five-hole pressure probes, and develops reduction equations for obtaining the desired aerodynamic parameters from raw data. It also presents comparison of hot-wire data using splitfilm probes and x-film probes collected during an airborne experiment.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1984
- Accession Number
- ADA146755
Entities
People
- W. C. Rose